VERFAHREN ZUM BESCHICHTEN EINER VERBUNDWERKSTOFFSTRUKTUR MIT EINER MEHRACHSIGEN KRISTALLINEN THERMOPLASTISCHEN BESCHICHTUNG

A method for thermoplastic coating composite structures includes applying a crystalline multi-axially oriented thermoplastic layer (14) onto a working surface (12) of a tool (10). A layer of composite material (16) is applied onto the crystalline multi-axially oriented thermoplastic layer (14), and...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	ANTON, DOM, WEIZENECKER, CHARLES, DIMARZIO, DON, CHU, STEVE
Format:	Patent
Sprache:	ger
Schlagworte:	ADHESIVES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING CHEMICAL PAINT OR INK REMOVERS CHEMISTRY COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS CORRECTING FLUIDS DYES FILLING PASTES INKS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM METALLURGY MISCELLANEOUS APPLICATIONS OF MATERIALS MISCELLANEOUS COMPOSITIONS NATURAL RESINS PAINTS PASTES OR SOLIDS FOR COLOURING OR PRINTING PERFORMING OPERATIONS POLISHES SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING USE OF MATERIALS THEREFOR WOODSTAINS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A method for thermoplastic coating composite structures includes applying a crystalline multi-axially oriented thermoplastic layer (14) onto a working surface (12) of a tool (10). A layer of composite material (16) is applied onto the crystalline multi-axially oriented thermoplastic layer (14), and the crystalline multi-axially oriented thermoplastic layer (14) and the layer of composite material (16) are cocured at a specific temperature and pressure in an autoclave. The softening temperature of the crystalline multi-axially oriented thermoplastic layer (!4) is not substantially greater than the curing temperature of the composite material (16). To be accompanied, when published, by Figure 1C of the drawings.